# Service difficulty reports: N67134

A list on [N67134](https://openairdocs.org/aircraft/N67134.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 86 reports

- [SDR CALA2026101920477](https://openairdocs.org/sdr/CALA2026101920477.md): Slide · unwanted deploy · Oct 16, 2026 · N67134 · Boeing 757224 · Escape Slide
  > DOOR 1L SLIDE DEPLOYED. REMOVED THE L1 EMERGENCY ESCAPE SLIDE AND GIRT BAR IAW AMM 25-66-01. REF LP 3781127 AND LP 377359 FOR WORK PERFORMED.
- [SDR CALA2026071617828](https://openairdocs.org/sdr/CALA2026071617828.md): Skin · cracked · Jul 16, 2026 · N67134 · Boeing 757224 · Wing, Plate/Skin
  > THE RT WING FUEL ACCESS OPENING (LWR WING SKIN) AT PANEL LOCATION 643BB, HAS A FASTENER HOLE (1EA) WITH A CRACK INDICATION AT THE 12 O'CLOCK POS AND (5EA) FASTENER HOLES WITH CORROSION INDICATIONS, SEE EA5720-03647 REV ORG FOR DAMAGE RESULTS AND LOCATION. REP
- [SDR CALA2026071217693](https://openairdocs.org/sdr/CALA2026071217693.md): Skin · dented · Jul 10, 2026 · N67134 · Boeing 757224 · Vertical Stabilizer, Plate/Skin
  > (SDR) LH VERTICAL STAB FIXED SKIN JUST BELOW APPROX FFS 119.467 HAS 1EA DENT. WC: 16068 SFR CW WSHAW ACCOMPLISHED REPAIR IAW SRM 51-70-10-2R-2 VIA PN 04-009-004 BATC H 4464640, RESTORED FINISH IAW SRM 51-21-14-370-803 & SRM 51-21- 15-370-801 PER SRM 55-30-01-2
- [SDR CALA2026071217691](https://openairdocs.org/sdr/CALA2026071217691.md): Skin · dented · Jul 10, 2026 · N67134 · Boeing 757224 · Vertical Stabilizer, Plate/Skin
  > LEFT VERTICAL STAB FIXED SKIN BETWEEN APPROX FSS 195.390 AND FSS 270.784 HAS 3EA DENT. ACCOMPLISHED REPAIR IAWSRM 51-70-10-2R-2 VIA PN 04-009-0044 BATC H 0004464640, RESTORED FINISH IAW SRM 51-21-14-370-803 & SRM 51- 21-15-370-801, PER SRM 55-30-01-2R-5 CLAS
- [SDR CALA2026071017648](https://openairdocs.org/sdr/CALA2026071017648.md): Skin · dented · Jul 8, 2026 · N67134 · Boeing 757224 · Leading Edge Devices
  > SLAT NR 2 UPPER SKIN HAS A DENT. REPAIRED THE NR 2 SLAT UPPER SKIN IAW SRM 51-70-10-2R-0.
- [SDR CALA2026070817606](https://openairdocs.org/sdr/CALA2026070817606.md): Angle · corroded · Jul 6, 2026 · N67134 · Boeing 757224 · Fuselage Main, Structure
  > RIGHT W/W BULKHEAD 1180, PANEL SUPPORT AT RBL 38.65 WAS CORRODED. REMOVED AND REPLACED 144N2503-136 ATTACHMENT VIA T26/1869249 AND 1442503104 ANGLE CLIP FABRICATED IAW SRM 51-40-02-0G AND SRM 51-40-05.
- [SDR CALA2026070517542](https://openairdocs.org/sdr/CALA2026070517542.md): Support Channel · broken · Jul 5, 2026 · N67134 · Boeing 757224 · Fuselage Miscellaneous Structure
  > RH W/W, STA 1060, LOWER SEAL RETAINER BRACKET IS BROKEN AT O/B SIDE. DOT 23-030. REF NR 16132. ESFR ENTRY ONLY FOR THE REPLACEMENT OF RETAINER. REMOVED AND REPLACED SUPPORT CHANNEL AT RT W/W STA 1060 IAW SRM 51-40-02-0G-0 AND DWG 149N7550.
- [SDR CALA2026070217527](https://openairdocs.org/sdr/CALA2026070217527.md): Support · corroded · Jul 1, 2026 · N67134 · Boeing 757224 · Wing Miscellaneous Structure
  > LH W/W, BULKHEAD 1180, PANEL SPRT BY LBL 16 AND LBL 31 IS CORRODED. REMOVED AND REPLACED 144N2503-135 ATTACH VIA T26/1869250 IAW SRM 51-40-02-0G. SRM 51-40-05. REMOVED AND REPLACED 144N2503-103 I AW SRM 51-40-02-0G VIA FABRICATION IAW 114N2503 REF DWG WITH 7
- [SDR CALA2026070117503](https://openairdocs.org/sdr/CALA2026070117503.md): Plate · corroded · Jul 1, 2026 · N67134 · Boeing 757224 · Fuselage Main, Plate/Skin
  > (EA 3830-01422 REV Q) AFT CARGO COMPT. AT STA. 1681.8 BILGE AREA, UPON REMOVAL BLADDER FOUND PLUG SKIN EXFOLIATED. REMOVED AND REPLACED PLATE ASSY-MOUNTING SUMP BLADDER, FLOOR DRA IN AT STA 1690 BTW STRG 29L TO 29R. IAW SRM 51-40-02- 0G0, DWG 417N2715 AND D
- [SDR CALA2026063017454](https://openairdocs.org/sdr/CALA2026063017454.md): Support Angle · cracked · Jun 28, 2026 · N67134 · Boeing 757224 · Nacelle/Pylon Miscellaneous Structure
  > AFT NR 2 PYLON PAN SKIN AFT INCONEL REMOVAL FOUND ANGLE WITH CRAC. REMOVED PAN SKIN ON NR 2 PYLON FOR ACCESS IAW SRM 51-41 -02-0G-0, REMOVED ANGLE ON PYLON NR 2 PAN SKIN AFT INCONEL IAW SRM 51-41-02-0G-0, LOCATED & DRILLED NEW SUPPORT ANGLE IAW SRM 51-41-05-0
- [SDR CALA2026063017452](https://openairdocs.org/sdr/CALA2026063017452.md): Support Bracket · cracked · Jun 28, 2026 · N67134 · Boeing 757224 · Wing Miscellaneous Structure
  > RIGHT WING, T/E REAR SPAR WS 313, SKIN PANEL SUPPORT BRACKET CRACKED AND WITH A FASTENER LOOSE. REMOVED DAMAGE BRACKET AT R/H WING THE REAR SPAR BY WS. 3/3 IAW SRM 51-40-02, RECIEVED NEW PART, LOCATED & DRILLED IAW SRM 51-40-05, TREATED AND PRIMED IAW AMM 51-
- [SDR CALA2026063017450](https://openairdocs.org/sdr/CALA2026063017450.md): Scuff Plate · cracked · Jun 28, 2026 · N67134 · Boeing 757224 · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR LOWER SEAL RETAINER LOWER FWD CORNER SUPPORT CRACKED. REMOVED AND RE-INSTALLED SCUFF PLATE FOR REPAIR AT THE WELD SHOP IAW EC/RA 5310-04203 PART 3 PARMANENT REPAIR WITH TRAVELER NR T26/1869222 AND AMM 53-13-02-424-005 ON FWD CARGO DOOR LOWER F
- [SDR CALA2026063017448](https://openairdocs.org/sdr/CALA2026063017448.md): Bracket · cracked · Jun 28, 2026 · N67134 · Boeing 757224 · Fuselage Miscellaneous Structure
  > MAIN DECK LEFT BS 1620 VERTICAL CEILING BRACKET CRACKED, 16274. FABRICATED BRACKET IAW DWG 411N3141 AND SRM 51-40-0 5-0G-0. TREATED AND PRIMED BRACKET IAW SRM 51-20-01-0G- 0.
- [SDR CALA2026062917389](https://openairdocs.org/sdr/CALA2026062917389.md): Angle · damaged · Jun 25, 2026 · N67134 · Boeing 757224 · Fuselage Miscellaneous Structure
  > LT MLG STRUCTURE THAT ATTACH 197AL AT BS 1040 HAS ANGLE BRACKET WITH A CRACK. REMOVED ANGLE BRACKET AT LH MLG STRUCTURE THAT ATTACH 197AL AT BS 1040 IAW SRM 51-40-02-0G-0, FABRICATED NEW ANGLE IAW DWG 149N7553 AND SRM 51-40-05-0G-0, APPLIED TREAT, PRIMER,
- [SDR CALA2026062917387](https://openairdocs.org/sdr/CALA2026062917387.md): Angle · cracked · Jun 25, 2026 · N67134 · Boeing 757224 · Aerodynamic Fairings
  > RT WING TO BODY SPRT ANGLE IS CRACKED AT BS 1040, RBL64, (BEHIND PANEL 198AR). REMOVED CLIP ANGLE AT RT WING TO BODY SUPPORT BS 1040, RBL 64, (BEHIND PANEL 198AR) IAW SRM 51-40-02-0G-0, FABRICATED NEW ANGLE, IAW DWG 149N7553 AND AMM 51-21-14-370-801, AMM 51
- [SDR CALA2026052616529](https://openairdocs.org/sdr/CALA2026052616529.md): Resistor · faulty · May 24, 2026 · N67134 · Boeing 757224 · Engine Indicating System Wiring
  > LEFT ENG EGT INOP AT CRUISE, WORKED IN DECENT PASSING F180. PER CONVERSATION WITH THE CREW, AFTER 4 HRS INTO FLIGHT, BOTH NORMAL & STBY EGT SHOWED 23 DEGREES & GOING THROUGH FL180 WHILE DESCENDING THE INDICATIONS CAME BACK TO NORMAL & REMAINED NORMAL ON LANDI
- [SDR CALA2026022414046](https://openairdocs.org/sdr/CALA2026022414046.md): Idg · faulted · Feb 23, 2026 · N67134 · Boeing 757224 · AC Generation System
  > RT AC BUSS OFF, FIGHT CREW REPORTED BUSS DROPPED OFF, CABIN WENT DARK AT TIME OF FAILURE AND DID WAS NOT PICKED UP. T/S IAW WDM 71-51-22-1 AND SSM 24-23-02. CHECKED WIRING FROM RT ENG GCU D2070B TO RT ENG IDG D1396P. ALL WIRING CHECKED GOOD. CHECKED RT ENG I
- [SDR CALA2026022013940](https://openairdocs.org/sdr/CALA2026022013940.md): Flap System · malfunctioned · Feb 19, 2026 · N67134 · Boeing 757224 · Trailing Edge Flap Control System
  > DURING APPROACH, TE FLAP DISAGREE BETWEEN FLAPS 25 TO 30. RETRACTED TO 20DRG GA AND EICAS CLRD INSPECTED LEADING EDGE AND TRAILING EDGE FLAPS NO DEFECTS NOTED. NO EICAS MESSAGE ON ARRIVAL.FLAPS OPERATE NORMALLY HYDRAULICALLY AND ELECTRICALLY. PERFORMED FSEU B
- [SDR CALA2025120411779](https://openairdocs.org/sdr/CALA2025120411779.md): Filter · faulted · Dec 1, 2025 · N67134 · Boeing 757224 · Turbine Engine Oil System
  > NUMBER 2 ENGINE VIBRATION REACHED 2.6 DURING CRUISE AT FL350, AMBER N1 CONDITI ON. RAN QRH, MAGNETIC CHIP DETECTORS INSPECTED, NO DISCREPENCIES FOUND IAW FIM 71-05, FAULT TREE 808 & AMM 79-00-00-216-001-R00. FOUND ECS MSG RT ENG BB VIB. & ON PERF/APU PAGE
- [SDR CALA2025111311168](https://openairdocs.org/sdr/CALA2025111311168.md): Light · broken · Nov 11, 2025 · N67134 · Boeing 757224 · Emergency Lighting
  > FOUND EMERGENCY EXIT PATH LIGHT PANEL BROKE ON ROW 32 ABC. ADJUSTED EMERGENCY EXIT PATH PANEL AS REQ, OPS CHECK GOOD. OK TO CONT.
- [SDR CALA2025110710988](https://openairdocs.org/sdr/CALA2025110710988.md): Bulb · inoperative · Nov 5, 2025 · N67134 · Boeing 757224 · Emergency Lighting
  > EMERGENCY LIGHTS LH WING EXIT FOUND LIGHT NOT ILLUMINATING REPLACED 2 BULBS PN 1317 REF 33-50-00.
- [SDR CALA2025090208354](https://openairdocs.org/sdr/CALA2025090208354.md): Girt Bar · loose · Aug 29, 2025 · N67134 · Boeing 757224 · Emergency Equipment
  > 4L DOOR WILL NOT ARM, DOOR 4L GIRT BAR AFT SENSOR COVER FOUND LOOSE, RESECURED. DOOR 4L SLIDE ARMING OPERATION TEST CARRIED OUT SATIS IAW AMM: 25-66-00 REV 137. LMC APPROVED TO REINSPECT L4 DOOR AFT GIRT BAR PROX SWITCH COVER FOR SECURITY. L4 DOOR AFT GIRT BA
- [SDR CALA2025082908284](https://openairdocs.org/sdr/CALA2025082908284.md): Cover · loose · Aug 27, 2025 · N67134 · Boeing 757224 · Emergency Equipment
  > 4L SLIDE LIGHT NOT ILLUM INATING WHEN DOOR IS ARMED. FOUND GIRT BAR SLIDER PROXIMITY SWITCH COVER LOOSE. SECURED THE PROTECTIVE COVER TO DOOR CUTOUT AND THRESHOLD IAW AMM 20-30-01-992-002. SLIDE ARMS WITH ARMED LIGHT ON.
- [SDR CALA2025082808211](https://openairdocs.org/sdr/CALA2025082808211.md): Slide · low pressure · Aug 25, 2025 · N67134 · Boeing 757224 · Escape Slide
  > DUE TO DOOR SLIDE AT 2L BEING SLOW TO INDICATE WITHIN THE GREEN BAND REPLACE THE 2L SLIDE IAW 25-66-01-401 CARRIED BY ELB REMOVED AND REPLACED L2 DOOR SLIDE PER AMM 25-66-01-404-044.NO FURTHER DEFECTS NOTED.ALL TESTS NORMAL AT THIS TIME. C/W RII INSPECTION OF
- [SDR CALA2025082208032](https://openairdocs.org/sdr/CALA2025082208032.md): Cooling Fan · faulted · Aug 20, 2025 · N67134 · Boeing 757224 · Air Distribution Fan
  > EQUIP COOLING OVERHEAT LIGHT ON SWITCH STATUS MSG EQPT CLG FAN, FOUND CB FWD EQUIP COOLING SUPPLY FAN TRIPPED,PUSHED BRAKER TRIPPED AGAIN.ALTN SWITCH WORKS OK. TRIPPING CB, MULTIPLE SYSTEMS ON C-B AND AN ELECTRICAL ODOR IN FLIGHT DECK UNLOCKED FOR SIGN OFF.
- [SDR CALA2025063006065](https://openairdocs.org/sdr/CALA2025063006065.md): Transducer · damaged · Jun 27, 2025 · N67134 · Boeing 757224 · Drag Control Actuator
  > SPOILERS CAUTION MSG DURING DESCENT POWER IDLE. SPOILERS DEPLOY ED WITH SLIGHT BANK RIGHTBITE OF SPOILER CONTROL MODULE 1, 2, AND 3 LEFT ALL SHOW SB LVDT FAULT, THAT ITS A HARD FAULT, AND ACTIVE. FLIGHT PHASE WAS ON GROUND. ALL 3 LEFT SCM'S FAULT D873, REF
- [SDR CALA2025051304637](https://openairdocs.org/sdr/CALA2025051304637.md): Annunciator · shorted · May 7, 2025 · N67134 · Boeing 757224 · Emergency Equipment
  > DOOR 2L WILL NOT DISARM MEL REQUESTED. APPROVED MEL 2566S COMPLIED WITH MX PROCEDURE, DOOR VERIFIED ARMED/GIRT BAR ENGAGED. SLIDE ARMED LIGHT DEF TO MEL. WITH SLIDE DISARMED, LIGHT STAYS LIT VERY DIM. *DM* SUGGEST AMM TASKS SYSTEM TEST 52-11-25-735-024 AND ADJ
- [SDR CALA2025040303477](https://openairdocs.org/sdr/CALA2025040303477.md): Bottle · within limits · Mar 31, 2025 · N67134 · Boeing 757224 · Escape Slide
  > DOOR 2L SLIDE PRESSURE GAUGE NOT IN GREEN. PRESSURE IS WITHIN LIMITS AS REF IN AMM REFERENCE: TASK 25-66-01-206-041NO. 1, 2, OR 4 PASSENGER DOOR ESCAPE SYSTEM CHECK. OK TO CONTINUE.
- [SDR CALA2025021300348](https://openairdocs.org/sdr/CALA2025021300348.md): Seat Track · corroded · Feb 12, 2025 · N67134 · Boeing 757224 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACKS - LEFT / OUTBOARD - CORROSION FOUND BETWEEN STA. 1080 AND STA. 1140 FABRICATED AND INSTALLED SEAT TRACK SECTION P/N 144N5021-4 REF DWG 144N5021 AND DWG 144N5001.SFR #3849957.
- [SDR CALA2025011700143](https://openairdocs.org/sdr/CALA2025011700143.md): Fan · failed · Jan 16, 2025 · N67134 · Boeing 757224 · Air Distribution Fan
  > AFTER PUSH HAD A SMOKY ODOR IN CABIN MAKERS IN USE AND OVENS OFF. NO VISABLE SMOKE REPORTED, ODOR OF SMELL DISSAPATED WHEN CABIN DOOR OPENED. DEBRIEFING FROM FLIGHT CREW. ODOR OF ELECTRICAL BURNING OCCURED IN ALL AREAS OF PASSENGER CABIN DURING PUSH BACK OFF G
- [SDR CALA2025011701940](https://openairdocs.org/sdr/CALA2025011701940.md): Unknown · odor · Jan 15, 2025 · N67134 · Boeing 757224 · Air Distribution System
  > COCKPIT AC AIR SMELLS LIKE DIRTY CARPETS. BA D. REF FIM21-00 TASK SUPPORT, FOUND ENGINE #1 OVER SERVICED WITH OIL, SUSPECT SMELL DUE TO OVER SERVICING OF ENGINE, RAN ENGINE, NO ABNORMAL SMELLS NOTED, OK FOR CONTINUED SERVICE.
- [SDR CALA2024103000971](https://openairdocs.org/sdr/CALA2024103000971.md): Girt Bar · fod · Oct 28, 2024 · N67134 · Boeing 757224 · Emergency Equipment
  > DOOR ARMED LIGHT ON DR 4L WENT OFF DURING FLIGHT. WAS ILLUMINATE D ON GROUND. REMOVED BOTTLE CAP FROM GIRT BAR ATTACH FITTING. DOOR 4L OP CK GOOD.
- [SDR CALA2024102900949](https://openairdocs.org/sdr/CALA2024102900949.md): Light · detached · Oct 26, 2024 · N67134 · Boeing 757224 · Emergency Lighting
  > 28C EMERGENCY ROW LT HANGING FROM HARNESS NEEDS SECURED RESECURED LIGHT, OPS CHECK GOOD, OK TO CONTINUE.
- [SDR CALA2024060301671](https://openairdocs.org/sdr/CALA2024060301671.md): Lamp · inoperative · May 30, 2024 · N67134 · Boeing 757224 · Emergency Lighting
  > EMER LIGHT NEAR AFT DOOR R NOT ON DURING TEST RELAMPED 767 BULB. WORKS OK NOW.
- [SDR CALA2024012900248](https://openairdocs.org/sdr/CALA2024012900248.md): Outflow Valve · erratic · Jan 26, 2024 · N67134 · Boeing 757224 · Pressure Regulator/Outflow Valve
  > CABIN ALT WARNING AT FL 380. CAB ALT INDICATED + 10000FT. OUT FL OW VALVE SHOWED FULL CLOSED. WHILE PERFORMING OUTFLOW VALVE TEST FOUND VALVE MOVEMENT ERRATIC WHEN COMMANDED. SUGGEST REPLACEMENT OF OUTFLOW VALVE PER 21-31-03-402-010. REMOVED AND REPLACED CABI
- [SDR CALA2023070302156](https://openairdocs.org/sdr/CALA2023070302156.md): Valve · leaking · Jun 30, 2023 · N67134 · Boeing 757200 · Engine Bleed Air System
  > IN FLIGHT AFTER TAKEOFF LEFT ENG OVHT WARNING TEST. TEST GOOD. LOCKING PG - MX TO CONTACT TOMC TO CLEAR FOUND NUMBER ONE ENGINE, INBOARD THRUST REVERSER, HYDRAULIC, HIGH ENGINE POWER RUN PERFORMED BY (R. BLASCHKE #093935) FAULT FLEXIBLE LINE. CHAFING ON NUMBER
- [SDR CALA2023062301997](https://openairdocs.org/sdr/CALA2023062301997.md): Door Seal · leaking · Jun 20, 2023 · N67134 · Boeing 757200 · Doors
  > DOOR 2 L LOUD SQUEAL DURING CLIMB TO CRUISE FL310 FOUND DIRT BUILDUP ON LOWER DOOR SEAL. CLEANED DEBRIS FROM LOWER DOOR SEAL. INSPECTED DOOR SEAL IAW AMM 52-09-01. NO RIPS OR TEARS NOTED
- [SDR CALA2023050301319](https://openairdocs.org/sdr/CALA2023050301319.md): Door · out of adjust · May 2, 2023 · N67134 · Boeing 757200 · Passenger/Crew Doors
  > R FWD ENTRY DOOR EICAS ON THEN FLASHES ON OFF WITH A/C MOVEMENT FAS SAY HNMDLE MOVING THERE ISNT MUCH OVER CENTER FORCE FELT. PERFORMED A VISUAL INSPECTION. FROM THE OUTSIDE THE DOOR AND HANDLE ARE FLUSH. FROM THE INSIDE THE IS NO DEBRIS IN OR AROUND THE FR
- [SDR CALA2023042101196](https://openairdocs.org/sdr/CALA2023042101196.md): Life Raft · damaged · Apr 20, 2023 · N67134 · Boeing 757200 · Life Raft
  > UPON RELOCATION OF THE OVERHEAD BIN DIVIDER FOUND THAT THE LIFE RAFT LOCATED IN OVERHEAD BIN AT 11ABC AREA TO BE UNRAVELED AT THE SURROUNDING SEAM. SUPPORT TASK NSA EMX N/R 00153. REMOVED AND REPLACED LIFE RAFT IN OVERHEAD BIN OFF P/N 63800-103 OFF S/N L5372 O
- [SDR CALA2023041901163](https://openairdocs.org/sdr/CALA2023041901163.md): Cover · unknown · Apr 17, 2023 · N67134 · Boeing 757 · Escape Slide
  > DURING SCHEDULED PARTS CHANGE FOR PART NUMBER 75-2561-9-0003 S/N 554 LEFT OFFWING EVACUATION SLIDE RELEASE CABLE NOT HOOKED UP. SUPPORT TASK NSA EMX N/R. 00169. REMOVED AND REPLACE LEFT OFF WING EVACUATION SLIDE IAW AMM 25-65-01. OFF P/N D31393-109 OFF S/N 055
- [SDR CALA2022111703163](https://openairdocs.org/sdr/CALA2022111703163.md): Line · loose · Nov 17, 2022 · N67134 · Boeing 757224 · Hydraulic Power Accumulator, Main
  > C HYD QTY STATUS MSG AT FL370 1 HOUR FROM LAN DING. FOLLOWED CHC KLIST ISOLATED SYS..43 RF FOUND RETURN LINE BETWEEN RT CTR PUMP AND EMP CASE DRAIN DUAL FILTER MODULE LOOSE. TIGHTENED FITTING PER AMM 29-00-98. SERVICED SYSTEM TO FULL PER AMM 12-12-01. LEAK CK
- [SDR CALA2022082602180](https://openairdocs.org/sdr/CALA2022082602180.md): None · none · Aug 26, 2022 · N67134 · Boeing 757 · Water and Waste System
  > WASTE DISPOSAL AFT LAV M - TOILET DOES NOT FLUSH AND RINSE SERVICED LAVS. OPS CHECK GOOD
- [SDR CALA2022030900609](https://openairdocs.org/sdr/CALA2022030900609.md): None · corroded · Mar 7, 2022 · N67134 · Boeing 757200 · Fuselage Structure (General)
  > L/H CREASE BEAM INNER CORD STA 755 TO 767 HAS CORROSION REF FLEE T CYCLE LOG PAGE 9805470. LOG PAGE CREATED FOR ESFR ONLY, SEE FLEET CYCLE L/P 9805470 FOR DETAILS OF WORK ACCOMPLISHED. REPAIRED INNER CHORD PER SRM 53-00-13-2R-1 REPAIR 1. LOG PAGE FOR ESFR ONLY
- [SDR CALA2022022800500](https://openairdocs.org/sdr/CALA2022022800500.md): None · corroded · Feb 23, 2022 · N67134 · Boeing 757200 · Fuselage Structure (General)
  > HEAVY CORROSION ON FLOOR DECK JUST FORWARD OF 1720 BULKHEAD FROM RBL 4.5 TO LBL 25. THIS LOGPAGE IS FOR ESFR TRACKING AND SUBMISSION ONLY. SEE FLEET CYCLE LOGPAGE 9803781 FOR WORK PERFORMED. COMPLETED ESFR FORM, SFR#1027819 DUE TO MAJOR REPAIR OF AFT FLOOR DEC
- [SDR CALA2021053100764](https://openairdocs.org/sdr/CALA2021053100764.md): Panel · detached · May 31, 2021 · N67134 · Boeing 757224 · Nacelle/Pylon, Plate/Skin
  > PDA 1 LP 6301347, #2 ENGINE, INBOARD PYLON PANEL DEPARTED AIRCRAFT ON LANDING @ RSW. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN INSTALL NEW PANEL, ARRIVES AT 20:05 FLT 0401 INSTALL NEW PANEL, ARRIVES AT 20:05 FLT 0401 UPDATED MAA CODE FIX USING VENDOR MAA SC
- [SDR CALA2019040100496](https://openairdocs.org/sdr/CALA2019040100496.md): Clamp · misinstalled · Mar 29, 2019 · N67134 · Boeing 757224 · Engine (Turbine/Turboprop)
  > FLIGHT CREW REPORTS AT 200'' AFTER TAKEOFF #2 ENGINE EGT RED EXCEEDANCE (931 DEG C) FOR 22 SEC FOLLOWED BY "R ENG OVHT" CAUTION FOLLOWED BY #2 ENGINE FIRE WARNING. FIRE HANDLE WAS PULLED, FIRE WARNING LIGHT EXTINGUISHED AND OVERHEAT CAUTION LIGHT OUT. BOTTLE W
- [SDR CALA2019031500421](https://openairdocs.org/sdr/CALA2019031500421.md): Skin · damaged · Mar 15, 2019 · N67134 · Boeing 757224 · Nacelle/Pylon, Plate/Skin
  > CUSTOMER REQUEST NO ENG PYLON HAS HEAT DAMAGE AT O/B SKIN JUST A BOVE T/R TO THE KEVLAR HEAT SHIELD (96-17) REF N/R 0058000 ACCOMPLISHED ECRA 5450-02555 REV- INTERIM REPAIR ON NR 2 PYLON O/B SIDE SKIN. WORK ACCOMPLISHED AND INSPECTED.
- [SDR CALA2019021100233](https://openairdocs.org/sdr/CALA2019021100233.md): Skin · cracked · Feb 8, 2019 · N67134 · Boeing 757224 · Passenger/Crew Doors
  > L4 INNER SKIN HAS MULTIPLE CRACKS AT UPPER HINGE AREA ABOVE KNUCKLE BUSTER ASSEMBLY. FOUND CRACKS OUT OF LIMITS IAW SRM 52-10-01-A1 L=.90, L =.65, L=.70. CUT OUT DAMAGE AND ACCOMPLISHED ECRA 5210-03004 REV - PM L4 DOOR INNER SKIN UPPER HINGE AREA. THIS IS TRAN
- [SDR CALA2019012800187](https://openairdocs.org/sdr/CALA2019012800187.md): Frame · dented · Jan 28, 2019 · N67134 · Boeing 757224 · Fuselage Main, Frame
  > DENT ON AFT CARGO FRAME UPPER FLANGE AT STA 1400 ABOVE STR 25L. AFT CARGO FRAME UPPER FLANGE DENT AT STA 1400 S-25L FOUND OUT OF LIMITS L=3.0, W=.85, D=.052 IAW SRM 53-00-07 FIG 101. CUT OUT DAMAGE AND ACCOMPLISHED PERMANENT REPAIR IAW SRM 53-00-07-R5.
- [SDR CALA2018121402566](https://openairdocs.org/sdr/CALA2018121402566.md): Warning Light · illuminated · Dec 11, 2018 · N67134 · Boeing 757224 · Leading Edge Slat Control System
  > LE SLAT DISAGREE LITE CAME ON GOING INTO LIH FOLLOWED QRH AND DI VERT TO HNL RAN FLAPS SLATS SEVERAL TIMES ON GRND CKS GOOD PERFORMED FSEU BITE NO PRESENT LEG FAULTS AND NO FAULT HISTORY A/C IS OK FOR SERVICE

Next page: https://openairdocs.org/aircraft/N67134/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N67134' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N67134/reports

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